RD-502

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RD-502

Part of RD-301

RD-502
NPO Enerogmash Museum, November 1992
Credit: © Dietrich Haeseler

Glushko H2O2/Pentaborane rocket engine. Experimental upper stage engine. Developed 1960-66. Experimental upper stage engine. Program stopped due to toxicity of propellants. Intended for Proton upper stage. First flight 1966.

Status: Developed 1960-66. Date: 1960-66. Thrust: 98.10 kN (22,054 lbf). Unfuelled mass: 132 kg (291 lb). Specific impulse: 380 s. Height: 2.51 m (8.23 ft). Diameter: 1.18 m (3.87 ft).

Initially proposed by Glushko for N-1 in September 1960.

Engine: 132 kg (291 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 75.75.

Family: Storable liquid. Country: Russia. Propellants: H2O2/Pentaborane. Agency: Glushko bureau. Bibliography: 317.

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